ELECTRICAL POWER SYSTEM FOR AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM

摘要

An electrical power system is disclosed for an aircraft having a hybrid-electric propulsion system, which includes a battery assembly for storing energy, an electric motor controller operatively connected to the battery assembly for conditioning and controlling power to an electric motor, and an electric motor receiving power through the motor controller for delivering torque to a shaft of the hybrid-electric propulsion system.